To provide a cabled flight vehicle capable of restraining moment of rotation of the flight vehicle from being generated by a tensile force of a cable.SOLUTION: A cabled flight vehicle 1 comprises: a flight vehicle 2 that has a plurality of lift generation parts 10 planarly arranged on a concentric circle, and a plurality of arm parts 20 extended toward the center C of the concentric circle from the plurality of lift generation parts 10; and a cable 3 that hangs down toward the ground from the flight vehicle 2. The cable 3 is connected to the flight vehicle 2, above a contact part B between the lift generation part 10 and the arm part 20, in the center C of the concentric circle.SELECTED DRAWING: Figure 1

    【課題】ケーブルの張力による飛行体の回転モーメントの発生を抑制することができる有線飛行体の提供。【解決手段】有線飛行体1は、同心円上に平面配置された複数の揚力発生部10と、複数の揚力発生部10から同心円の中心Cに向かって延びる複数のアーム部20と、を有する飛行体2と、飛行体2から地上に向かって垂れ下がるケーブル3と、を備え、ケーブル3は、同心円の中心Cにおいて、揚力発生部10とアーム部20との接点部Bよりも上部で、飛行体2に接続されている。【選択図】図1


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    Titel :

    CABLED FLIGHT VEHICLE


    Weitere Titelangaben:

    有線飛行体


    Beteiligte:

    Erscheinungsdatum :

    10.09.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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